View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 59688U 26145.51469601 +.00000000 +00000-0 -60466-4 0 00006
2 59688 43.0055 335.4675 0001179 264.7175 95.3543 15.27578732 04
| Epoch (UTC): | 25 May 2026 12:21:09 |
| Eccentricity: | 0.0001179 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.4675° |
| argument of perigee: | 264.7175° |
| revolutions per day: | 15.27578732 |
| mean anomaly at epoch: | 95.3543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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